[0001] The invention relates to an air flow meter according to the first portion of claim
1 for measuring the flow rate of intake air supplied to an internal-combustion engine
of an automobile or the like.
[0002] There are several known methods for measuring the flow rate of intake air supplied
to an internal-combustion engine. Among them, heat-sensitive air flow meters, such
as hot-wire air flow meters, are widely employed, since they are generally excellent
in responsiveness and capable of measuring the mass flow rate. Such heat-sensitive
air flow meters are known from US-A-3,747,577, US-A-3,750,632 and US-A-3,824,966.
These known heat sensitive air flow meters are arranged such that as a flow rate sensing
part of platinum wire with a diameter of from 70 µm to 100 um is stretched inside
an intake pipe. This arrangement, however, is insecure in durability and easily mechanically
damaged by a backfire occurring particularly when the internal-combustion engine is
in a bad condition.
[0003] In order to cope with these disadvantages it is known from the US-A-4,264,961 that
a part of the air passing through an intake pipe is introduced into a bypass pipe,
in which a platinum wire is mounted. However, such a by-pass pipe type air flow meter
has a binary problem. The binary problem is a phenomenon that a heat-sensitive air
flow meter indicates the same output value although the flow rates of intake air are
different from each other.
[0004] This binary problem arises in the full-load operation range of an internal-combustion
engine.
[0005] In the EP-A-0082484 (publication date 29.06.1983) is disclosed an air flow meter
for the suction system of an internal-combustion engine having a flow rate detector
disposed in a by-pass passage. The by-pass passage communicates with a pressure-accumulating
chamber, in which the pressure of the backward gas flow will be stored. This pressure
serves as a flowing resistance with respect to the airflow in the by-pass passage
during the succeeding forward air flow condition.
[0006] An air flow meter assembly according to the EP-A-0054887 (publication date 30.06.1982)
belongs to the prior art in which a hot wire element is disposed in a by-pass air
passage. The by-pass air passage is provided to prolong a distance of length between
the inlet opening of the by-pass passage and the hot-wire, thereby to settle the flow
of air in the by-pass passage at least in the area around the hot-wire. The inlet
opening of the by-pass air passage may open in a plane perpendicular to the axis of
the venturi portion and within the area of upper projection of the venturi portion,
to prevent carbon and oil particles from coming into the by-pass passage thereby to
prevent the contamination of the hot-wire.
[0007] From the DE-A-29 14 275 it is known an air flow meter according to the first portion
of claim 1 comprising a venturi in the manifold on the upstream side of the throttle
flap and an air flow sensor element of the thermosensitive type, which is disposed
in a by-pass air passage. The inlet opening of a first straight portion of the by-pass
passage directed in parallel to the venturi of the main passage is disposed on the
upstream side of the venturi. The straight passage portion is connected with a second
portion of the by-pass passage formed as a ring channel in the body of the main passage
and having at least one outlet opening formed as a slot and disposed in the smallest
area of the venturi.
[0008] In this air flow meter the whole length of the by-pass passage is not exactly fixed,
since the air flows out through the outlet slot extending over a substantial portion
of the circumference of the venturi. For this reason also by this type of air flow
meter it exists the binary problem.
[0009] The object of the invention is to provide a by-pass type air flow meter according
to the preamble of claim 1 which has no binary problem.
[0010] The solution of this object is defined by the characterizing features of claim 1.
Description of the drawings:
[0011]
Fig. 1 is a characteristic graph showing the relationship between the manifold pressure
and the output voltage in a conventional heat-sensitive air flow meter;
Fig. 2 is a chart schematically showing the relationship between the manifold pressure
and the output voltage in the air flow meter shown in Fig. 1;
Figs. 3 and 4 illustrate problems of the prior art, respectively;
Figs. 5 to 9 illustrate the principle of the present invention, respectively;
Fig. 10 is a partly sectioned side elevational view of a preferred embodiment of the
invention;
Fig. 11 is a partly sectioned plan view of the embodiment shown in Fig. 10;
Fig. 12 illustrates the flow rate of the air in a by-pass passage in a blow-back state;
Fig. 13 is a plan view of a further preferred embodiment of the invention; and
Fig. 14 is a partly sectioned side elevational view of the embodiment shown in Fig.
13.
Description of the preferred embodiments:
[0012] Fig. 1 is a graph illustrating the relationship between the manifold pressure and
the flow sensing signal (output voltage) in a conventional heat-sensitive air flow
meter for internal-combustion engines. The manifold pressure represented by the horizontal
axis substantially corresponds to the throttle opening. Consequently, the higher the
manifold pressure (as it goes rightwards as viewed in Fig. 1), the larger the throttle
opening. Moreover, curves in Fig. 1 show characteristics at constant engine speeds,
respectively: the curve A at 1000 RPM; the curve B at 1200 RPM; the curve C at 1400
RPM; the curve D at 1600 RPM; the curve E at 1800 RPM; the curve Fat 2000 RPM; the
curve G at 2400 RPM; the curve H at 2800 RPM; the curve I at 3200 RPM; the curve J
at 3600 RPM; the curve K at 4000 RPM; the curve L at 4400 RPM; and the curve M at
4800 RPM.
[0013] In Fig. 1, the characteristic curves have a tendency to droop in the shape of the
elephant trunk in the regions close to the totally open state of the throttle, particularly
at low speed, from 1000 RPM to 2000 RPM and at high speed, above 4000 RPM. Consequently,
there is a binary problem that the values of output (V) of the flow sensing signal
are the same although manifold pressures, i.e., intake air flow rates are different
from each other.
[0014] Such a binary problem leads the intake air flow rate sensing signal to have a large
error, so that it becomes impossible to effect an accurate engine control.
[0015] Fig. 2 is a chart schematically illustrating one of characteristics showing the relationship
between the manifold pressure and the air flow in the heat-sensitive air flow meter
shown in Fig. 1. As the throttle opening becomes larger and the manifold pressure
becomes higher, intake pulsations are generated. The zone A shown by an arrow includes
regions where intake pulsations are noticeably generated, while the zone B shown by
an arrow includes regions where blow-back takes place particularly remarkably in the
intake pulsation regions. Assuming that the straight line shown by a solid line is
a real air flow line, the air flow obtained from the output of a heat-sensitive probe
shows a characteristic illustrated by a series of circles. In the zone A, the output
signal of the heat-sensitive probe showing the air flow iowers, causing an error to
become larger. Moreover, in the zone B, being affected by the blow-back, the output
signal becomes larger than the real value, leading to a positive error.
[0016] The relationship between the air flow and the output signal is nonlinear as shown
by a solid line in Fig. 3. Therefore, in the case where the air flow passing through
the air flow meter is a pulsating flow as shown by a solid line A, the output signal
of the flow meter varies as shown by a solid line B. Consequently, when the output
signal is averaged per period of the pulsation and an air flow Q
1 is obtained from the averaged signal V
1, the air flow Q
1 is smaller than an average value Q
2 of the real air flow. As a result, the relationship between the real air flow and
the air flow (measured value) obtained from the above-mentioned averaged value in
case of varying the intake pipe pressure under a condition
' of a constant engine speed is such as shown in Fig. 2. Namely, in engine operation
regions where the intake pulsation has a large pulsation amplitude, measured values
become smaller than real air flows, leading to large measuring errors. Moreover, the
result obtained by means of a computer simulation is shown in Fig. 4 with the amplitude
ratio of pulsation represented by the horizontal axis.
[0017] If the average air flow rate is denoted by U
o, while the amplitude ratio of the pulsating flow is designated by A, the flow rate
U of the pulsating air flow is represented by the following formula:

[0018] The amplitude ratio A means the proportion of the amplitude of the pulsation to the
average value U
o.
[0019] In Fig. 4, the horizontal axis represents the amplitude ratio A of the pulsating
flow. When the amplitude ratio A is 1, the amplitude is maximum and equal to U
o. On the other hand, the vertical axis represents the ratio between a real air flow
and a value measured by the flow meter. When the ratio is 0 the real air flow and
the measured value coincide with each other. It will be understood that the larger
the amplitude ratio A of pulsation, the smaller the measured value than the real value,
causing a measuring error to enlarge.
[0020] Fig. 5 illustrates the principle of a heat-sensitive air flow meter according to
the invention, which is schematically shown in order to facilitate theoretical calculation.
A heat-sensitive probe 4 is disposed in a by-pass passage 5 formed in a throttle body
1 and having an inlet 6 provided on the upstream side of a Venturi part 3 in a main
intake passage 2 and an outlet 8 provided at the Venturi part 3. Now if the pressure
at the inlet 6 is denoted by p
i, while the pressure at the outlet 8 is designated by p
2, the pressure difference p,-p
2 produced when intake pulsation is generated is represented by the following formula:

where L is the length between two planes perpendicular to the air flow in the main
passage 2, one of which includes the inlet 6 of the by-pass passage 5 and the other
includes the center of the outlet 8 thereof.
p is the air density;
ε is a frictional loss coefficient;
A, is the sectional area of the main intake passage at the Venturi part 3;
A2 is the sectional area of the by-pass passage 5; and
u2 is the air flow rate in the main intake passage at a section 8.
[0021] On the other hand, the air flow rate w in the by-pass passage resulting from the
pressure difference p,-p
2 is represented by the following formula:

where I is the length of the by-pass passage. It is to be noted that the first term
on the right side of each of the above formulae (2), (3) represents the inertia of
the air flow.
[0022] Fig. 6 is a chart showing the calculation results of the air flow rate w in the by-pass
passage in case of sinusoidally varying the air flow rate u
2 in the main intake passage at the outlet 8 of the by-pass passage. In other words,
the amplitude of w shown by a solid line is decreased as compared with that of u
2 shown by a broken line because of an inertial lag effect. In addition, owing to a
Venturi effect between the main intake passage at sections 6 and 8 in Fig. 5, i.e.,
the relationship shown by p
1xp
2xu
22, the average value w tends to become larger than u
2.
[0023] Fig. 7 shows this with respect to the amplitude ratio A of pulsation by means of
computer simulation, similarly to Fig. 4. The larger the amplitude ratio A of pulsation,
and the larger the iength I of the by-pass passage, the larger the by-pass passage
average air flow rate than the main passage average air flow rate. In this case, the
length L of the main passage is 30 mm.
[0024] Fig. 8 is a chart showing a characteristic obtained by means of the by-pass passage
shown in Fig. 5, where the horizontal axis represents values of I/L, while the vertical
axis represents values of wfü
z. In other words, by properly selecting I/L, it becomes possible to cancel the decrease
in the flow meter output in the regions in the zone A of Fig. 2 where intake pulsation
is noticeably generated, by the increase in the average flow rate in the by-pass passage
due to the inertial lag effect.
[0025] Fig. 9 shows the output error with respect to the ratio of the by-pass passage length
I to the main passage length L, I/L, when the internal-combustion engine is operated
at 1000 RPM with the throttle totally open. It will be apparent from Fig. 9 that the
error becomes small so that it can be practically neglected if the ratio of the by-pass
passage length to the main passage length between the branching part and the combining
part is 3 or more.
[0026] In other words, when the ratio is 3, the error is -5%, and such a small error will
not cause a binary problem although the measured value is smaller than the actual
air flow as shown by a dash and dotted line in Fig. 2. When the ratio is 5 or more,
the error becomes positive. However, a positive error will not cause a binary problem,
since in such a case the measured value is larger than the actual air flow. It is
to be noted that the measured value becomes larger than the actual air flow in the
blow-back regions in the zone B in Fig. 2, as shown by a dash and dotted line, since
the effect obtained by lengthening the by-pass passage is small in such regions.
[0027] Referring to Figs. 10 and 11 showing a preferred embodiment of the invention respectively,
the parallel by-pass passage 18 is formed inside the side wall part of the main passage
16 so as to be parallel thereto. A pipe 60 forming an outer peripheral by-pass passage
is connected to the lower end of the parallel by-pass passage 18. An outlet end 62
of the pipe 60 is connected to an opening 64 opened in the side wall of the main passage
16. In other words, an inlet end 66 of the pipe 60 is connected to the lower end of
the parallel by-pass passage 18, and the pipe 60 is disposed so as to surround substantially
all the periphery of the side wall part of the main passage 16 as well as combine
with the main passage 16 again through the outlet end 62. In this embodiment, the
the outer peripheral by-pass passage is formed by the pipe 60 mounted on the outside
of the main passage side wall part.
[0028] A part of the intake air flowing in through the air cleaner is made to branch off
and flow in from the inlet end of the parallel by-pass passage 18 and passed through
the heat-sensitive resistors 20, 22 before flowing into the pipe 60 forming the outer
peripheral by-pass passage. After travelling round substantially all the periphery
of the main passage 16, the part of the intake air reenters the main passage 16 from
the opening 64.
[0029] According to the above-described embodiment, it is possible to enlarge the inertia
of the intake air flow in the by-pass passage, since the outer peripheral by-pass
passage is connected to the downstream end of the parallel by-pass passage 18 parallel
to the main passage 16 for lengthening the length of the by-pass passage. Therefore,
even when intake pulsation is generated by the engine operation, it is possible to
decrease the amplitude of the pulsation in the by-pass passage, thereby making it
possible to maintain the state of flow relatively close to the steady flow. Thus,
since the intake air flow in the by-pass passage, i.e., the flow in the passage where
the heat-sensitive resistor 20 is disposed is made close to the stationary state,
thereby allowing the pulsation to be smaller, it is possible to decrease the responsive
lag effect of the sensing signal representative of the flow sensed by the heat-sensitive
resistor 20. Accordingly, it is possible to resolve the binary problem due to the
above-mentioned responsive lag (particularly the responsive lag in rising), i.e.,
the binary problem based on that only an average flow lower than the actual flow can
be sensed owing to the fact that the responsive lag becomes larger in rising although
there is a small responsive lag in decaying.
[0030] Moreover, according to the above-described embodiment, since the outer peripheral
by-pass passage 60 is provided at the portion surrounding the main passage 16, all
of the by-pass passage can be housed within the range of the heat-sensitive flow meter.
Accordingly, it is possible to obtain a heat-sensitive flow meter for internal-combustion
engines with a simple and compact structure and having no binary problem.
[0031] In addition, in the case of forming the by-pass passage by the by-pass passage parallel
to the main passage and the by-pass passage formed on the outer periphery of the main
passage as shown in the above-described embodiment, the length of the by-pass passage
can be made substantially three or more times longer than that of the main passage
by making the length of the outer peripheral by-pass passage two or more times longer
than that of the parallel by-pass passage.
[0032] As will be apparent from the above description, according to the embodiment of the
invention, the binary problem arising when pulsation is generated is resolved, and
the characteristic such as shown by the dash and dotted line in Fig. 2 can be obtained.
However, the measured value is larger than the actual flow in the blow-back regions
in the zone B as shown by the dash and dotted line in Fig. 2.
[0033] Fig. 12 is a chart showing the air flow rate in the by-pass passage measured when
blow-back takes place. A curve
U2 shown by a solid line represents the intake air flow rate in the main passage at
the outlet of the by-pass passage, while a curve w shown by a broken line represents
the air flow rate in the by-pass passage 18. In a region x where a back flow is produced
when blow-back occurs, even when the main passage air flow rate
U2 is negative, the air flow rate w in the by-pass passage having an enlarged I/L is
positive. Therefore, if such a method is employed that the waveform of w shown by
the broken line is held from being positive as much as possible by applying the dynamic
pressure of the back flow of the main passage air to the outlet of the by-pass passage
in the regions x, the air flow rate in the by-pass passage approachs zero, so that
it is possible to obtain a characteristic such as shown by a dash and dotted line.
Thus, the dash and dotted line in the zone B in Fig. 2 further approaches ideal values
shown by the solid line, thereby allowing the air flow rate error to be decreased.
[0034] Figs. 13 and 14 show a further preferred embodiment of the invention respectively.
Fig. 13 is a plan view, while Fig. 14 is a partly sectioned side elevational view
of the embodiment shown in Fig. 13. In this embodiment, a heat-sensitive air flow
meter and a throttle valve 82 are formed into a unitary structure. According to this
arrangement, the ratio between the air flow rates in the main and by-pass air passages
16, 18 is easily affected by the throttle valve opening. It is desirable for coping
with this disadvantage to allow the direction of the by-pass passage outlet 64 to
coincide with the axial direction of a throttle valve shaft 88.
[0035] Moreover, a wire mesh 86 for preventing the entry of dust is provided on the upstream
side of the main air passage 16 and the by-pass air passage 18. In a by-pass type
flow meter, the length of the resistors 20, 22 is obliged to be short, since the diameter
of the by-pass air passage 18 is smaller than that of the main air passage 16. Further,
if the inlet of the by-pass air passage 18 is opened in the direction of the air flow
as illustrated, when, for example, a part of elements of the air cleaner peels off,
it easily enters the by-pass air passage and may cover a part of the resistors 20,
22. Since the length of the resistors 20, 22 is short as mentioned above, even if
only a part thereof is covered, there will be a large change in the signal obtained
therefrom. Therefore, the flow meter with such an arrangement as illustrated needs
at the inlet thereof the wire mesh for preventing the entry of dust. Although the
mesh of the wire mesh should be as small as possible from the viewpoint of prevention
of the entry of dust, as the mesh is made smaller, the breathing resistance undesirably
becomes larger. Therefore, a required mesh is about the length of the resistor 20,
and a mesh of from 0.5 to 2 mm is preferable.
[0036] As the electric circuit it is possible to employ such a bridge circuit as mentioned
in US-A-3,747,577.
1. Air flow meter for a suction system of an internal combustion engine having:
a main passage (16) provided between an air cleaner and the internal combustion engine;
a Venturi (14) provided in the main passage (16) on the upstream side of a throttle
valve (83);
a by-pass passage (18) having an inlet opening to the main passage (16) disposed on
the upstream side with respect to the Venturi (14) and an outlet (64) to the Venturi
(14); and
an air flow sensor (20, 22) provided in the by-pass passage (18), characterized in
(a)-that the width of the outlet opening of the by-pass passage (18) in the circumferential
direction is very small in comparison to the inner circumference of the main passage
(16);
(b)-that the direction of the outlet (64) and the direction of the shaft (88) of the
throttle valve (83) coincide with each other, and
(c)-that the ratio I/L of the length (I) of the by-pass passage (18) to the length
L of a part of the main passage (16) is substantially 3 or more, wherein the length
L is the distance between two planes crossing the main passage (16) perpendicularly
to the flow direction, one of which including the inlet opening and the other including
the center of the outlet opening of the by-pass passage (18).
2. Air flow meter as defined in claim 1, characterized in that the by-pass passage
(18) includes a straight portion parallel to the main passage (16) and a curved portion
(60) formed on the outer periphery of the main passage (16).
3. Air flow meter as defined in claim 2, characterized in that the by-pass passage
(18) is formed in the wall of a body (10) constituting the main passage (16) and that
the outlet (64) is a slot.
4. Air flow meter as defined in claim 3, characterized in that the body constituting
the main passage (16) is composed of at least two members (10, 12), one (10) of said
two members having therein a portion of the main passage (16) and the straight portion
of the by-pass passage (18), the other having the rest of the main passage (16), at
least one (10) of said two members (10, 12) having a groove formed around the outer
periphery of the main passage (16), so that by connecting the two members the curved
portion of the by-pass passage (18) will be formed at the connection of the two members.
5. Air flow meter as defined in claim 2, characterized in that the curved portion
of the by-pass passage (18) is formed by a pipe (60), the outlet (64) of which is
in the member constituting the main passage (16).
6. Air flow meter as defined in claim 1, characterized in that the by-pass passage
(18) is adapted to take in the air flowing in through the air cleaner by a dynamic
pressure.
7. Air flow meter as defined in claim 1, characterized in that the by-pass passage
(18) is adapted to take in the air flowing in through the air cleaner by a static
pressure.
8. Air flow meter as defined in claim 1, characterized in that a member for preventing
the entry of dust is provided on the upstream side of the inlet opening of the by-pass
passage (18).
9. Air flow meter as defined in claim 2, characterized in that the length of the curved
portion is two or more times longer than that of the straight portion of the by-pass
passage (18) and in that the air flow sensor (20) is provided in the straight portion.
1. Luftdurchflußmengenmesser für ein Ausaugsystem einer Brennkraftmaschine mit:
einer zwischen einem Luftfilter und der Brennkraftmaschine liegenden Hauptleitung
(16);
einem in der Hauptleitung (16) aufstrom von einer Drosselklappe (83) befindlichen
Lufttrichter (14);
einer Bypassleitung (18), die eine Einlaßöffnung zur Hauptleitung (16) in der Aufstromseite
des Lufttrichters (14) und einen Auslaß (64) zum Lufttrichter (14) aufweist; und
einem Luftdurchsatzmengenfühier (20, 22) in der Bypassleitung (18), dadurch gekennzeichnet,
(a) daß die Weite der Auslaßöffnung der Bypassleitung (18) in Umfangsrichtung sehr
klein ist im Vergleich zum Innenumfang der Hauptleitung (16);
(b) daß die Richtung des Auslasses (64) und die Richtung der Welle (88) der Drosselklappe
(83) übereinstimmen, und
(c) daß das Verhältnis I/L der Länge (I) der Bypassleitung (18) zur Länge L eines
Teils der Hauptleitung (16) im wesentlichen 3 oder mehr beträgt, wobei die Länge L
der Abstand zwischen zwei die Hauptleitung (16) senkrecht zur Strömungsrichtung kreuzenden
Ebenen ist, wobei die eine Ebene die Einlaßöffnung und die andere Ebene die Mitte
der Auslaßöffnung der Bypassleitung (18) einschließt.
2. Luftdurchflußmengenmesser nach Anspruch 1, dadurch gekennzeichnet, daß die Bypassleitung
(18) einen zur Hauptleitung (16) parallelen geraden Abschnitt und einen am Außenumfang
der Hauptleitung (16) gebildeten gekrümmten Abschnitt (60) aufweist.
3. Luftdurchflußmengenmesser nach Anspruch 2, dadurch gekennzeichnet, daß die Bypassleitung
(18) in der Wand eines die Hauptleitung (16) bildenden Körpers (10) gebildet und daß
der Auslaß (64) ein Schlitz ist.
4. Luftdurchflußmengenmesser nach Anspruch 3, dadurch gekennzeichnet, daß der die
Hauptleitung (16) bildende Körper aus wenigstens zwei Teilen (10, 12) besteht, wobei
in dem einen Teil (10) ein Abschnitt der Hauptleitung (16) und der gerade Abschnitt
der Bypassleitung (18) und in dem anderen Teil die restliche Hauptleitung (16) vorgesehen
sind, wobei wenigstens einer (10) der beiden Teile (10, 12) eine um den Außenumfang
der Hauptleitung (16) verlaufende Nut aufweist, so daß durch Verbinden der beiden
Teile der gekrümmte Abschnitt der Bypassleitung (18) an der Verbindungsstelle zwischen
den beiden Teilen gebildet ist.
5. Luftdurchflußmengenmesser nach Anspruch 2, dadurch gekennzeichnet, daß der gekrümmte
Abschnitt der Bypassleitung (18) durch ein Rohr (60) gebildet ist, dessen Auslaß (64)
sich in dem die Hauptleitung (16) bildenden Teil befindet.
6. Luftdurchflußmengenmesser nach Anspruch 1, dadurch gekennzeichnet, daß die Bypassleitung
(18) so ausgebildet ist, daß sie die durch den Luftfilter einströmende Luft durch
dynamischen Druck ansaugt.
7. Luftdurchflußmengenmesser nach Anspruch 1, dadurch gekennzeichnet, daß die Bypassleitung
(18) so ausgebildet ist, daß sie die durch den Luftfilter einströmende Luft durch
statischen Druck ansaugt.
8. Luftdurchflußmengenmesser nach Anspruch 1, dadurch gekennzeichnet, daß ein Element,
das den Eintritt von Staub hemmt, aufstrom von der Einlaßöffnung der Bypassleitung
(18) vorgesehen ist.
9. Luftdurchflußmengenmesser nach Anspruch 2, dadurch gekennzeichnete daß die Länge
des gekrümmten Abschnitts zwei- oder mehrfach länger als diejenige des geraden Abschnitts
der Bypassleitung (18) und daß der Luftdurchflußmengenfühler (20) im geraden Abschnitt
angeordnet ist.
1. Débitmètre d'air pour un système d'aspiration d'un moteur à combustion interne
comportant:
un passage principal (16) disposé entre un filtre à air et le moteur à combustion
interne;
un venturi (14) prévu dans le passage principal (16) sur le côté amont d'un papillon
des gaz (83);
un passage de dérivation (18) possédant une ouverture d'admission débouchant dans
le passage principal (16) et située sur le côte amont par rapport au venturi (14),
et une sortie (64) débouchant dans le venturi (14); et
un capteur (20, 22) du débit d'air, disposé dans le passage de dérivation (18), caractérisé
en ce que
(a)―ta largeur de l'ouverture de sortie du passage de dérivation (18) dans la direction
circonférentielle est très faible par rapport à la circonférence intérieure du passage
principal (16);
(b)-la direction de la sortie (64) et la direction de l'arbre (88) du papillon des
gaz (83) coïncident entre elles, et
(ε)Ie rapport I/L de la longueur (I) du passage de dérivation (18) à la longueur
L d'une partie du passage principal (16) est égal sensiblement à 3 ou plus, la longueur
L étant la distance entre deux plans recoupant le passage principal (16) perpendiculairement
à la direction d'écoulement, l'un de ces plans incluant l'ouverture d'entrée et l'autre
incluant le centre de l'ouverture de sortie du passage de dérivation (18).
2. Débitmètre d'air selon la revendication 1, caractérisé en ce que le passage de
dérivation (18) comporte une partie rectiligne parallèle au passage principal (16)
et une partie courbe (60) formée sur le pourtour extérieur du passage principal (16).
3. Débitmètre d'air selon la revendication 2, caractérisé en ce que le passage de
dérivation (18) est formé dans la paroi d'un corps (10) constituant le passage principal
(16) et que la sortie (64) est une fente.
4. Débitmètre d'air selon la revendication 3, caractérisé en ce que le corps constituant
le passage principal (16) est constitué par au moins deux éléments (10, 12), dont
l'un (10) contient en lui une partie du passage principal (16) et la partie rectiligne
du passage de dérivation (18) et dont l'autre contient le reste du passage principal
(16), au moins l'un (10) desdits deux éléments (10,12) possédant une gorge disposée
sur le pourtour extérieur du passage principal (16) de sorte que, sous l'effet du
raccordement des deux éléments, la partie courte du passage de dérivation (18) est
formée au niveau de la zone de raccordement des deux éléments.
5. Débitmètre d'air selon la revendication 2, caractérisé en ce que la partie courbe
du passage de dérivation (18) est constituée par un conduit (60), dont la sortie (64)
est située dans l'élément constituant le passage principal (16).
6. Débitmètre d'air selon la revendication 1, caractérisé en ce que le passage de
dérivation (18) est adapté pour recevoir l'air pénétrant dans le filtre à air sous
l'effet d'une pression dynamique.
7. Débitmètre d'air selon la revendication 1, caractérisé en ce que le passage de
dérivation (18) est adapté pour recevoir l'air pénétrant dans le filtre à air sous
l'effet d'une pression statique.
8. Débitmètre d'air selon la revendication 1, caractérisé en ce qu'un élément servant
à empêcher la pénétration de la poussière est prévu sur le côte amont de l'ouverture
d'entrée du passage de dérivation (18).
9. Débitmètre d'air selon la revendication 2, caractérisé en ce que la longueur de
la partie courbe est deux ou plusieurs fois supérieure à celle de la partie rectiligne
du passage de dérivation (18) et en ce que le capteur (20) du débit d'air est disposé
dans la partie rectiligne.